2021 Vol. 47, No. 12

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Volume 47 Issue122021
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Dual-linear-array TFM ultrasonic imaging method for weld defects of complex structure
ZHOU Zhenggan, TENG Lichen, LI Yang
2021, 47(12): 2407-2413. doi: 10.13700/j.bh.1001-5965.2020.0464
Abstract:

A certain type of superalloy disk component of aero-engine is welded by the turbine disk and the outer integral blade ring, and when the conventional single-channel ultrasonic method is used to detect welding surface defects, there are problems such as low detection resolution and poor signal-to-noi...

A multi-model centralized storage method for embedded system
YAN Zhipeng, CAI Xingquan, YANG Bo, WU Ji
2021, 47(12): 2414-2425. doi: 10.13700/j.bh.1001-5965.2020.0501
Abstract:

The software safety is important factor in our daily life, model-driven software development gains more and more attention. For the existing integration barriers of cross-domain models, we popose a method based on meta-modeling techniques, which is applied for extracting multi-perspective model info...

Air traffic CPS cascading failure and mitigation strategy
WANG Xinglong, HE Min, LIU Mingxue
2021, 47(12): 2426-2433. doi: 10.13700/j.bh.1001-5965.2020.0466
Abstract:

To effectively alleviate the cascading failure of air traffic, the traditional load-capacity model is improved, and the critical value of capacity adjusting parameter is discovered. An air traffic Cyber Physical System (CPS) model is built, and its nodes are defined to be in three states: normal, co...

Fatigue life prediction of aluminum alloy with pre-corrosion damage based on damage mechanics
ZHAN Zhixin, YU Xun, HU Weiping, MENG Qingchun
2021, 47(12): 2434-2441. doi: 10.13700/j.bh.1001-5965.2020.0477
Abstract:

In engineering structures, the corrosion fatigue failure is a common phenomenon. The fatigue crack often occurs around the corrosion pit, which seriously affects the fatigue characteristics of materials. In this paper, based on the continuous damage mechanics, a method is proposed for the fatigue li...

Behavioral decision learning reward mechanism of unmanned swarm system
ZHANG Tingting, LAN Yushi, SONG Aiguo
2021, 47(12): 2442-2451. doi: 10.13700/j.bh.1001-5965.2020.0600
Abstract:

Unmanned swarm system is composed of a multi-agent system, which can meet task requirements through autonomous and cooperative behavior. The instability of agent training is increased because agents adopt behavior and change states autonomously. In this paper, the prior constraints and the isomorphi...

Supportability evaluation of aviation equipment system based on uncertainty
CUI Lijie, CONG Jiping, DING Gang, REN Bo, WANG Yi, LI Jihong
2021, 47(12): 2452-2461. doi: 10.13700/j.bh.1001-5965.2020.0490
Abstract:

Aimed at the characteristics of complex structure, various elements, and strong coupling of aviation equipment system, based on the analysis of its support process, the multi-Agent modeling technology is used to carry out the supportability modeling of the aviation equipment system, and analysis and...

Principle and application of airspace spatial grid identification
ZHU Yongwen, PU Fan
2021, 47(12): 2462-2474. doi: 10.13700/j.bh.1001-5965.2020.0487
Abstract:

At present, in the related researches of airspace spatial finite element, the construction of a grid identification system for airspace space is an important foundation for applying information technology to airspace management and promoting airspace digitization. Based on the US military's global r...

Robust nonlinear flight control method against control saturation
SUN Bing, CHEN Wei
2021, 47(12): 2475-2483. doi: 10.13700/j.bh.1001-5965.2020.0473
Abstract:

When the aerocraft is maneuvering in a large envelope, its rudder surface and engine are easily saturated. This phenomenon will not only affect the stability of the closed-loop system, but also greatly shorten the service life of the engine and other key components. To solve this problem, a nonlinea...

Experimental and computational study on blade surface pressure measurement of coaxial rigid rotor in hovering state
JIANG Lusheng, CAO Yaxiong, LIU Ting, FAN Feng
2021, 47(12): 2484-2493. doi: 10.13700/j.bh.1001-5965.2020.0669
Abstract:

For the coaxial rigid model rotor in hovering state, the experimental and numerical simulation research on blade surface pressure measurement were carried out. The micro pressure sensor was used to measure the blade surface pressure, which not only obtains the experimental data of blade surface pres...

Effect of alertness light environment on flight cognitive task performance
CHEN Yanhao, YU Suihuai, CHU Jianjie, CUN Wenzhe
2021, 47(12): 2494-2502. doi: 10.13700/j.bh.1001-5965.2021.0124
Abstract:

The effects of monochromatic blue light and three groups of blue-enriched light on the change of alert level of flight cognitive tasks were tested from the subjective and objective performance of flight cognitive tasks. Objective experimental evaluation, including the measurement of flight main and ...

Real-time performance optimization of TTE network based on "pay bursts only once" principle
ZHENG Zhong, ZHAO Luxi, HE Feng, XIONG Huagang, LU Guangshan
2021, 47(12): 2503-2513. doi: 10.13700/j.bh.1001-5965.2020.0415
Abstract:

The development of deterministic communication promotes the introduction of time-triggered concepts. Time-Triggered Ethernet (TTE) network supports real-time applications of mixed safety by providing three traffic classes, including Time-Triggered (TT) traffic, which has complete time certainty, Rat...

Theoretical and experimental study on synthesis of high-content catocene
LIU Xiaoju, SUO Qi, FENG Haitao, ZHANG Chi, MA Xiaoyan
2021, 47(12): 2514-2520. doi: 10.13700/j.bh.1001-5965.2020.0497
Abstract:

2, 2'-bis (ethylferrocenyl) propane (catocene) is a kind of high-efficiency burning rate liquid catalyst with excellent comprehensive performance. It is a mixture with four isomers of the different substituting positions of ethyl groups and other different substitutions of diferrocenyl propane compo...

Aerodynamic characteristics of airfoil near wavy water surface
HU Haode, MA Dongli, YANG Muqing, GUO Yang
2021, 47(12): 2521-2532. doi: 10.13700/j.bh.1001-5965.2020.0448
Abstract:

The aerodynamic characteristics of NACA 4412 airfoil moving over wavy water at small clearance is studied by solving Navier-Stokes equations. The accuracy of the numerical method is verified. The aerodynamic coefficients of airfoil moving over wavy water surface and wavy ground are calculated and co...

High-resolution network Anchor-free object detection method based on iterative aggregation
WANG Xin, LI Zhe, ZHANG Hongli
2021, 47(12): 2533-2541. doi: 10.13700/j.bh.1001-5965.2020.0484
Abstract:

In order to solve the problems of inaccuracy in heat map generation and insufficient detection accuracy of anchor-free object detection method CenterNet (Objects as Points), a high-resolution representation network CenterNet-DHRNet based on feature iterative aggregation is proposed. First, for the p...

Remaining useful life prediction method based on random coefficient regression model with imperfect prior information
WAN Changhao, LIU Zhiguo, TANG Shengjin, SUN Xiaoyan, SI Xiaosheng
2021, 47(12): 2542-2551. doi: 10.13700/j.bh.1001-5965.2020.0439
Abstract:

Remaining Useful Life (RUL) prediction is a core problem of equipment prognostics and health management. Accurate RUL prediction can make effective maintenance management before the failure occurs to reduce the probability of equipment failure. A heuristic RUL prediction method is proposed to overco...

Effects of capsule wake on parachute working performance
WU Zhuoheng, YU Li, ZHAO Xiaoshun, NIE Shunchen
2021, 47(12): 2552-2559. doi: 10.13700/j.bh.1001-5965.2020.0465
Abstract:

To study the unsteady effects of capsule wake on parachute aerodynamic performance, the Realizable k-ε turbulence model and PISO algorithm are used to calculate the unsteady flow around the capsule-parachute system, and an accurate flow field vortex structure is obtained. The research on the variati...

Intelligent design method of landing gear retraction and extension trajectory for narrow space
ZHU Linhao, ZOU Zehua, YIN Yin, LIU Xiangyang, CAI Xinzhi
2021, 47(12): 2560-2570. doi: 10.13700/j.bh.1001-5965.2020.0440
Abstract:

The flattened aerodynamic shape is the preferred layout for hypersonic vehicles to obtain high lift drag ratio, but this shape seriously restricts the collection space of the landing gear, and the conventional mechanism is difficult to meet the requirements. Engineers can only use the three-dimensio...

G1-variation-coefficient-KL based TOPSIS radar jamming effectiveness evaluation
LI Zhijun, XIANG Jianjun, SHENG Tao, XIAO Bingsong
2021, 47(12): 2571-2578. doi: 10.13700/j.bh.1001-5965.2020.0493
Abstract:

When jamming effectiveness evaluation is transformed to a multi-attribute decision-making problem, traditional Technique for Order Preference by Similarity to an Ideal Solution (TOPSIS) is too objective to fully reflect the will of the evaluator, and the method only considers the inter-index Euclide...

A chicken swarm optimization algorithm based on improved X-best guided individual and dynamic hierarchy update mechanism
ZHANG Kewei, ZHAO Xiaolin, HE Li, LI Zongzhe
2021, 47(12): 2579-2593. doi: 10.13700/j.bh.1001-5965.2020.0322
Abstract:

In the improvement process of swarm intelligence algorithms, elite individuals are often used to accelerate the convergence, but excessive dependence on them will lead to the decline of population diversity and global convergence. In this regard, a chicken swarm optimization algorithm based on impro...

Parameter determination method of relative small crack growth rate formula in durability analysis
ZUO Randong, HE Xiaofan, LI Yuhai
2021, 47(12): 2594-2601. doi: 10.13700/j.bh.1001-5965.2020.0492
Abstract:

Relative small crack growth rate formula of structural details is the key to durability analysis using probabilistic fracture mechanics method. In order to determine the applicable range and parameters of the formula, it is necessary to carry out group fatigue tests under multiple stress levels, whi...

Dynamic modeling and simulation of morphing vehicle
YAN Qimin, HU Junhua, CHEN Guoming, LIU An, ZHANG Qiang
2021, 47(12): 2602-2610. doi: 10.13700/j.bh.1001-5965.2020.0496
Abstract:

In view of the problem that the dynamic model of some morphing vehicles is complex, which is caused by the complicated variant description and the rigid-flexible coupling, a general applicable dynamic equation of morphing vehicle is derived. The vehicle is regarded as a whole composed of mass points...

Analysis of accumulation effect of turntable bearing and its influence on rotary performance
DENG Biao, CHEN Jianwei, GUO Yang, TANG Shengjin, CHEN Wei
2021, 47(12): 2611-2622. doi: 10.13700/j.bh.1001-5965.2020.0499
Abstract:

In order to solve the problem of friction moment increase caused by rolling body accumulation during the rotating process of the space launch pad turntable bearing, this paper studied the influence of the change of clearance between the rolling bodies on the rolling. Based on the finite element anal...

Reconstruction of sparse parity-check matrix of LDPC codes based on iterative decoding
ZHONG Zhaogen, LIU Renxin, ZHANG Limin, DAN Bo, LIU Jie
2021, 47(12): 2623-2631. doi: 10.13700/j.bh.1001-5965.2020.0500
Abstract:

In order to improve the performance of Low Density Parity Check (LDPC) code sparse parity-check matrix reconstruction algorithm under high error rate, this paper proposes a sparse parity-check matrix reconstruction algorithm based on the idea of iterative decoding. First, the dual space algorithm is...

Lightweight identity authentication protocol based on dynamic ID in multi-server environment
QI Xiaochen, LI Meihong, DU Ye
2021, 47(12): 2632-2640. doi: 10.13700/j.bh.1001-5965.2020.0442
Abstract:

To realize the communication security and efficient identity authentication between users and servers, how to design effective identity authentication protocols has gradually become an important research hotspot, more and more identity authentication protocols are proposed. First, this paper analyse...

Control moment characteristics of double-jet circulation control airfoil
HE Yujuan, LEI Yuchang, ZHANG Dengcheng, ZHANG Yanhua, ZHOU Zhangwen
2021, 47(12): 2641-2649. doi: 10.13700/j.bh.1001-5965.2021.0080
Abstract:

In order to study the possibility of flight control by circulation control technology, the control moment characteristics of steady jet circulation control airfoil in steady flow field are studied. The aerodynamic coefficient variation rules of virtual rudder and traditional rudder produced by singl...

High-altitude floating mechanism and vertical trajectory simulation of double-layer latex balloon
HE Hong, ZHU Huajian, SHEN Zhipeng, XIAO Di'e, PAN Xianzhi, LI Fanzhu
2021, 47(12): 2650-2656. doi: 10.13700/j.bh.1001-5965.2020.0505
Abstract:

The double-layer latex balloon overcomes the shortcomings of the single-layer latex balloon and can float at high altitude with long time to achieve continuous meteorological observation. However, its high-altitude floating mechanism influenced by multiple factors is much more complicated. In partic...